ASTM F3236-21a PDF
Standard Specification for High Intensity Radiated Field (HIRF) Protection in Small Aircraft
Standard Specification for High Intensity Radiated Field (HIRF) Protection in Small Aircraft
- Статус документа:
- Действующий
- Формат:
- Электронный (PDF)
- Количество страниц:
- 5
- Дата публикации:
- 1 ноября 2021 г.
- Издание:
- F3236
- ICS:
- 49.020
ABSTRACT This specification applies to the high intensity radiated field (HIRF) protection aspects of airworthiness and design for ”small” aircraft. It establishes the Aircraft Type Code (ATC) compliance matrix based on airworthiness level, number of engines, type of engine(s), stall speed, cruise speed, meteorological conditions, altitude, and maneuvers. An ATC is defined by taking into account both the technical considerations regarding the design of the aircraft and the airworthiness level established based upon risk-based criteria. The requirements described by this specification for HIRF protection cover electrical and electronic systems that perform a function whose failure would prevent the continued safe flight and landing of the aircraft; electrical and electronic systems that perform a function whose failure would significantly reduce the capability of the aircraft or the ability of the flight crew to respond to an adverse operating condition; and the HIRF environments and equipment HIRF test levels for electrical and electronic systems. SCOPE 1.1 This specification covers international standards for the high intensity radiated field (HIRF) protection aspects of airworthiness and design for “small” aircraft. 1.2 The applicant for a design approval must seek the individual guidance for their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their Small Aircraft Airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM F44 webpage (www.astm.org/committeee/F44.htm), which includes CAA website links. Annex A1 maps the Means of Compliance described in this specification to EASA CS-23, amendment 5, or later, and FAA 14 CFR Part 23, amendment 64, or later. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.4 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.
Abstract
Overview
ASTM F3236-21a – Standard Specification for High Intensity Radiated Field (HIRF) Protection in Small Aircraft defines international standards for ensuring that small aircraft are adequately protected against high intensity radiated fields (HIRF). By outlining requirements for the design and airworthiness of electrical and electronic systems, this ASTM standard helps safeguard critical flight operations from electromagnetic interference, which poses a significant risk to aircraft safety. The specification applies to aircraft of various types and operating conditions and is aligned with major aviation authority regulations such as those from the FAA and EASA.
Key Topics
- HIRF Protection Requirements: The standard establishes criteria for protecting essential electrical and electronic systems that are vital for the continued safe flight and landing of small aircraft.
- Assessment Matrix: A compliance matrix based on Aircraft Type Code (ATC) takes into account airworthiness level, engine details, aircraft speeds, operating environment, altitude, and maneuvers to determine appropriate protection levels.
- System Design: Electrical and electronic systems must be designed to prevent failure when exposed to defined HIRF environments, including the ability to recover function automatically after exposure where operationally feasible.
- Test Environments: Several HIRF environments and test levels are identified, with specific field strength values and susceptibility test methods, ensuring comprehensive electromagnetic protection across a broad frequency spectrum.
- International Alignment: The standard harmonizes with EASA CS-23 and FAA 14 CFR Part 23 regulations, providing mapped means of compliance to regulatory requirements.
Applications
- Aircraft Certification & Compliance: ASTM F3236-21a is essential for any manufacturer or operator seeking certification of small aircraft, both new and retrofitted, to prove compliance with HIRF protection rules as required by civil aviation authorities.
- Design Guidance for Engineers: The standard offers engineers a clear framework when designing or modifying electrical and electronic systems in small aircraft, ensuring that critical avionics maintain performance under electromagnetic interference conditions.
- Integration Into Certification Plans: Applicants must coordinate with their respective civil aviation authorities to use this specification as an accepted means of compliance within their certification plans, ensuring adherence to local and international regulations.
- Risk Mitigation: By following ASTM F3236-21a, operators and designers reduce the risk of electromagnetic events causing system failures, thereby enhancing passenger and crew safety.
Related Standards
- ASTM F3060: Establishes terminology for aircraft, supporting clear interpretation of requirements in F3236-21a.
- ASTM F3061/F3061M: Covers systems and equipment specifications for small aircraft, including definitions and compliance guidance referenced in the HIRF protection standard.
- EASA CS-23: European certification standard for normal, utility, aerobatic, and commuter aeroplanes, with cross-referenced requirements in this ASTM specification.
- FAA 14 CFR Part 23: U.S. airworthiness standards for normal category airplanes, providing the regulatory basis for much of the HIRF protection guidance.
- EUROCAE ED-107 and SAE ARP 5583: Industry-recognized guides for certifying aircraft in HIRF environments, offering complementary methodologies and technical reference points.
Keywords: HIRF protection, high intensity radiated field, small aircraft, airworthiness, electromagnetic interference, ASTM F3236-21a, electrical system protection, aircraft certification.
Технические детали
- Технический комитет
- F44 - General Aviation Aircraft
- SKU
- ASTM F3236-21a
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